基于自适应模糊神经网络的弹药消耗预计模型

根据我军弹药消耗预计方法的现状,利用模糊控制和神经元网络原理,提出了一种新的预计方法。量化的作战条件作为系统的输入,预计值作为系统的输出,根据历史的输入、输出数据确定系统的特性,建立预计模型。利用此种方法建立的模型根据历史数据训练后,输入现有战斗估计条件,即可对部队日平均作战消耗做出预计。     

基于SFS的磨粒图像三维重构

研究了一种由磨粒灰度图像直接恢复出磨粒图像三维信息的磨粒三维形貌恢复方法，以几种典型的磨粒灰度图像进行算法验证，实验结果表明，该方法简单，易于实现，恢复后的磨粒三维图像有较强的立体感。在不增加硬件成本的基础上，可以为磨粒的分析提供三维数据，为磨粒图像三维特征的提取奠定基础，对磨粒识别精度的提高产生重要的影响。     

多约束下的高超声速飞行器三维非线性自适应末制导律

面向多约束下高超声速飞行器末制导过程中的通道耦合、参数扰动、模型失配等突出问题,设计一种适于高超声速飞行器的三维非线性自适应末制导律。为了模型描述的完整性和简洁性,引入视线旋量和旋量速度的概念,并基于此建立三维制导参考模型和实际系统的表达式;为了保证制导律的鲁棒性和自适应性,基于自适应控制理论,设计一种三维非线性自适应制导律;通过数学推导证明了该制导律的稳定性。该制导律能够从理论上克服高超声速飞行器末制导面临的通道耦合、参数扰动、模型失配等突出问题,满足多约束制导要求。仿真结果验证了所设计制导律的有效性。     

Consequence of reinforced SiC particles and post process artificial ageing on microstructure and mechanical properties of friction stir processed AA7075

Friction stir processing and post process artificial ageing was successfully carried out on AA7075 with and without reinforcement of SiC particles producing defect free processed zone with uniform distribution of filler material. Effect of SiC particle reinforcement and artificial ageing times on the microstructural modifications was characterized using optical and electron microscopy, electron backscattered diffraction and X-Ray diffraction. Hardness, impact and wear tests were carried out to investigate mechanical behaviour before and after processing. Reinforcement of SiC particles during FSP and subsequent age hardening treatment brought about nearly twofold increase in hardness and impact toughness values by the combined effect of grain refinement, Zener pinning, dispersion strengthening and precipitation hardening. Significant improvement in wear resistance in terms of wear loss was also observed after processing compared to the reference material AA7075-T6. Fractured surface of post FSP age hardened AA7075 alloy exhibited features of ductile fracture during Charpy impact test.     

基于GPS+GLONASS观测的高精度、快速定位与定向试验

在现代战争中 ,导弹发射阵地的高精度、快速定位与定向是实现灵活机动作战 ,有效地打击敌方目标 ,保障野外实战生存能力的需要。首先 ,重点论述快速构筑导弹发射阵地的实施过程以及GPS +GLONASS组合系统的数据处理方法。最后 ,通过使用连续 2 4h的观测数据分段试验计算 ,结果表明 :利用GPS +GLONASS组合系统 ,在 2 0min时间内可以完成对导弹发射阵地的高精度定位、定向任务     

美“海军一体化火力控制--制空”能力发展现状与启示

美“海军一体化火力控制－制空”（ NIFC－CA）是美军海上盾牌防御体系概念的重要组成部分。该体系经过多年的发展已初见成效。首先，对美“海军一体化火力控制———制空”的基本概念及内涵进行了阐述，对其主要组成CEC、E－2D预警机、宙斯盾系统及标准－6舰空导弹在防御体系中的功能进行了分析；然后，介绍了美NIFC－CA的6种主要指挥控制模式，并对其协同指挥决策模式进行了分析，得出了指挥决策分布处理的特点；最后，总结了美NIFC－CA发展对我海军海上防御力量发展建设的启示。     

一种传感器网格自协同作战模型*

传统的协同技术不能满足传感器网格复杂的协同应用在动态性、实时性以及分布决策的强协同等方面的需求。为此,建立了一种自协同技术,给出了自协同作战虚拟组织(ACBVO)的参量化描述,提出了传感器网格自协同作战模型(SGACBM),描述了协同成员的信息结构和功能结构。使用SGACBM,ACBVO能在执行任务过程中,不断监测协同工作的质量,并根据协同质量动态切换协同机制。SGACBM能改善传感器网格的协同质量,加速作战进程,实现传感器网格自协同作战。     

一种面向目标的伪彩色图像融合算法

针对远距离红外与可见光融合图像中目标不突出的问题,提出了一种面向目标的伪彩色图像融合算法。基于目标特征将红外图像分割为目标区域和背景区域,以人类视觉的生物机理和感受野的数学模型为基础,利用差分高斯函数(Difference of Gaussians,DOG)模拟视觉拮抗特性,对目标区域和背景区域用改进的感受野模型和不同的彩色映射规则进行伪彩色图像融合。实验结果显示:该算法能够保留图像共有特征,突出独有特征,融合图像色彩自然、目标突出,具有良好的视觉效果。     

三关节机器人的神经网络补偿自适应控制器设计

三关节机器人广泛用于工业生产、轮式或履带式排爆机器人,为了补偿由于机器人结构参数、作业环境干扰等不确定性因素造成的机器人动力学模型的不确定性,将机器人动力学模型分解为名义模型和误差模型两部分,其误差模型采用RBF神经网络进行补偿,得到其估计信息,神经网络的输出权值根据Lyapunov稳定性理论采用自适应算法进行调整。所设计的神经网络补偿自适应控制器解决了不确定性机器人动力学系统控制器设计的不确定性问题,同时,通过定义Lyapunov函数,证明了控制器能渐近、稳定地跟踪期望轨迹。机器人的3个关节在控制器的作用下,约在5 s时达到期望轨迹,神经网络约在5 s时逼近机器人动力学模型的误差模型,实验结果表明了机器人关节对期望轨迹具有良好的轨迹跟踪性能。     

Investigation on the spatial distribution characteristics of behind-armor debris formed by the perforation of EFP through steel target

The behind-armor debris (BAD) formed by the perforation of an EFP is the main damage factor for the secondary destruction to the behind-armor components. Aiming at investigating the BAD caused by EFP, flash X-ray radiography combined with an experimental witness plate test method was used, and the FEM-SPH adaptive conversion algorithm in LS-DYNA software was employed to model the perforation process. The simulation results of the debris cloud shape and number of debris were in good agreement with the flash X-ray radiographs and perforated holes on the witness plate, respectively. Three-dimensional numerical simulations of EFP's penetration under various impact conditions were conducted. The results show that, an ellipsoidal debris cloud, with the major-to-minor axis radio (a/b) smaller than that caused by shaped charge jets, was formed behind the target. With the increase of target thickness (h) and decrease of impact velocity (v₀) and obliquity (θ), the value of a/b decreases. The number of debris ejected from target is significantly higher than that from EFP. Based on the statistical analysis of the spatial distribution of the BAD, An engineering calculation model was established considering the influence of h, v₀ and θ. The model can with reasonable accuracy predict the quantity and velocity distribution characteristics of BAD formed by EFP.